Problems of commuter airplane configuration design were studied to affect a minimization of direct operating costs. Factors considered were the minimization of fuselage drag, methods of wing design, and the estimated drag of an airplane submerged in a propellor slipstream; all design criteria were studied under a set of fixed performance, mission, and stability constraints. Configuration design data were assembled for application by a computerized design methodology program similar to the NASA-Ames General Aviation Synthesis Program.


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    Titel :

    A study of commuter airplane design optimization


    Beteiligte:
    Roskam, J. (Autor:in) / Wyatt, R. D. (Autor:in) / Griswold, D. A. (Autor:in) / Hammer, J. L. (Autor:in)

    Erscheinungsdatum :

    31.08.1977


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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